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1-series cowling-spinner combinations 1-series open-nose cowlings absolute coefficient angle of attack boundary layer calculated conical spinner cowling and spinner cowling length cowling lip cowlings and cowling-spinner Critical inlet-velocity ratio critical Mach number d/Dc decrease design conditions design critical Mach determined by separation effect of spinner envelope values equation Fioure flight Mach number flow separation Fmure function of inlet-velocity higher inlet-velocity ratios inlet area inlet diameter inlet lip inlet-diameter ratio inner lip internal flow knee Langley Aeronautical Laboratory Langley Field locate minimum design Mach number characteristics Mach number curve mass-flow coefficient minimum design values minimum inlet-velocity ratio NACA 1-series cowling-spinner NACA 1-series cowlings NACA 1-series spinners NACA spinner number and inlet-velocity obtained PoFVo predicted critical Mach pressure coefficients pressure recovery Propeller installed propeller operation Propeller removed separation from spinners spinner diameter spinner proportions spinner surface surface pressure distributions test Mach number Ticks locate minimum value of inlet-velocity velocity ratio X/Dc